Effects of Size of External Stores on the Aerodynamic Characteristics of an Unswept and a 45© Sweptback Wing of Aspect Ratio 4 and a 60© Delta Wing at Mach Numbers of 1.41, 1.62, and 1.96 PDF Download

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Effects of Size of External Stores on the Aerodynamic Characteristics of an Unswept and a 45© Sweptback Wing of Aspect Ratio 4 and a 60© Delta Wing at Mach Numbers of 1.41, 1.62, and 1.96

Effects of Size of External Stores on the Aerodynamic Characteristics of an Unswept and a 45© Sweptback Wing of Aspect Ratio 4 and a 60© Delta Wing at Mach Numbers of 1.41, 1.62, and 1.96 PDF Author: Carl R. Jacobsen
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 62

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Book Description

Effects of Size of External Stores on the Aerodynamic Characteristics of an Unswept and a 45© Sweptback Wing of Aspect Ratio 4 and a 60© Delta Wing at Mach Numbers of 1.41, 1.62, and 1.96

Effects of Size of External Stores on the Aerodynamic Characteristics of an Unswept and a 45© Sweptback Wing of Aspect Ratio 4 and a 60© Delta Wing at Mach Numbers of 1.41, 1.62, and 1.96 PDF Author: Carl R. Jacobsen
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 62

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Book Description

Effects of the Spanwise, Chordwise, and Vertical Location of an External Store on the Aerodynamic Characteristics of a 45 Degree Sweptback Tapered Wing of Aspect Ratio 4 at Mach Numbers of 1.41, 1.62, and 1.96

Effects of the Spanwise, Chordwise, and Vertical Location of an External Store on the Aerodynamic Characteristics of a 45 Degree Sweptback Tapered Wing of Aspect Ratio 4 at Mach Numbers of 1.41, 1.62, and 1.96 PDF Author: Carl R. Jacobsen
Publisher:
ISBN:
Category :
Languages : en
Pages : 31

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Book Description

Effects of Systematically Varying the Spanwise and Vertical Location of an External Store on the Aerodynamic Characteristics of an Unswept Tapered Wing of Aspect Ratio 4 at Mach Numbers of 1.41, 1.62, and 1.96

Effects of Systematically Varying the Spanwise and Vertical Location of an External Store on the Aerodynamic Characteristics of an Unswept Tapered Wing of Aspect Ratio 4 at Mach Numbers of 1.41, 1.62, and 1.96 PDF Author: Carl R. Jacobsen
Publisher:
ISBN:
Category :
Languages : en
Pages : 34

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Book Description

Effects of Overhang Balance on the Hinge-moment and Effectiveness Characteristics of an Unswept Trailing-edge Control on a 60 Degree Delta Wing at Transonic and Supersonic Speeds

Effects of Overhang Balance on the Hinge-moment and Effectiveness Characteristics of an Unswept Trailing-edge Control on a 60 Degree Delta Wing at Transonic and Supersonic Speeds PDF Author: Lawrence D. Guy
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 52

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Book Description
A wind-tunnel investigation has been made of two unswept, partial-span, flap-type controls (differing only in hinge-line location) mounted on a 60 degree delta wing. One control was unbalanced and the other has a 100-percent overhang balance. Control hinge moments as well as aerodynamic characteristics of the complete wing-body combination were obtained for control deflections from 0 to 40 degrees over an angle-of-attack range of plus or minus 12 degrees at Mach numbers from 0.75 to 1.96. Reynolds numbers varied between 2,200,000 and 2,200,000. Expressions derived from linear theory for the hinge-moment coefficient due to angle of attack for unswept partial-span controls (which extend neither to the wing tip nor to the wing center line) on triangular wings having subsonic leading edges are given in an appendix.

Aerodynamic Loading Characteristics in Sideslip of a 45© Sweptback Wing with and Without a Fence at High Subsonic Speeds

Aerodynamic Loading Characteristics in Sideslip of a 45© Sweptback Wing with and Without a Fence at High Subsonic Speeds PDF Author: Richard E. Kuhn
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 50

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Book Description

Wind-tunnel Investigation of the Effects of Steady Rolling on the Aerodynamic Loading Characteristics of a 45© Sweptback Wing at High Subsonic Speeds

Wind-tunnel Investigation of the Effects of Steady Rolling on the Aerodynamic Loading Characteristics of a 45© Sweptback Wing at High Subsonic Speeds PDF Author: James W. Wiggins
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 32

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Book Description

An Analysis of the Effects of Wing Aspect Ratio and Tail Location on Static Longitudinal Stability Below the Mach Number of Lift Divergence

An Analysis of the Effects of Wing Aspect Ratio and Tail Location on Static Longitudinal Stability Below the Mach Number of Lift Divergence PDF Author: John A. Axelson
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 20

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Book Description
An analysis is presented of the influence of wing aspect ratio and tail location on the effects of compressibility upon static longitudinal stability. The investigation showed that the use of reduced wing aspect ratios or short tail lengths leads to serious reductions in high-speed stability and the possibility of high-speed instability.

A Tabulation of Wind-tunnel Pressure Data and Section Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.01 for Two Trapezoidal and Three Delta Wings Having Different Surface Shapes

A Tabulation of Wind-tunnel Pressure Data and Section Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.01 for Two Trapezoidal and Three Delta Wings Having Different Surface Shapes PDF Author: Emma Jean Landrum
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 76

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Book Description

Wind-tunnel Investigation at Low Speed of the Effect of Varying the Ratio of Body Diameter to Wing Span from 0.1 to 0.8 on the Aerodynamic Characteristics in Pitch of the 45© Sweptback-wing--body Combination

Wind-tunnel Investigation at Low Speed of the Effect of Varying the Ratio of Body Diameter to Wing Span from 0.1 to 0.8 on the Aerodynamic Characteristics in Pitch of the 45© Sweptback-wing--body Combination PDF Author: Harold S. Johnson
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36

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Book Description

Transonic Wind-tunnel Investigation of the Effects of Sweepback and Thickness Ratio on the Wing Loads of a Wing-body Combination of Aspect Ratio 4 and Taper Ratio 0.6

Transonic Wind-tunnel Investigation of the Effects of Sweepback and Thickness Ratio on the Wing Loads of a Wing-body Combination of Aspect Ratio 4 and Taper Ratio 0.6 PDF Author: Robert J. Platt
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 50

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Book Description
A transonic investigation of the effects of sweepback and thickness ratio on the wing loads of a wing in the presence of a body has been made in the Langley 8-foot transonic pressure tunnel. The tests covered wings with a thickness ratio of 6 percent for sweepback angles of 0, 25, and 45 degrees and a thickness ratio of 4 percent for an unswept wing.